Search Results

Standard

Direction Instrument, Non-Magnetic, Stabilized Type (Directional Gyro)

2012-08-22

CURRENT

AS397B

This Aeronautical Standard covers two basic types as follows: Type I - Air Operated Type II - Electrically Operated

Standard

Direction Instrument, Magnetic (Stabilized Type)

2012-08-22

CURRENT

AS399B

This Aeronautical Standard covers minimum requirements for gyroscopically stabilized Magnetic Direction Instruments for use in aircraft.

Standard

Flight Directors (Turbine-Powered Subsonic Aircraft)

2012-08-22

CURRENT

AS406A

This standard covers flight directors for use on aircraft to indicate to the pilot, by visual means, the correct control application for the operation of an aircraft in accordance with a preselected flight plan.

Standard

Compass; Magnetic, Pilot's Standby

2012-08-22

CURRENT

AS5604A

This specification covers the design requirements and all performance requirements for procurement of 1 7/8 inch dial pilot’s standby compasses as specified herein.

Standard

TUBE - PITOT, ELECTRICALLY HEATED

2012-08-22

CURRENT

AS5813A

Standard

Automatic Pilots

2012-08-22

CURRENT

AS402C

This Aeronautical Standard covers Automatic Pilots intended for use on aircraft to automatically operate the aerodynamic controls to maintain flight and/or to provide maneuvering about the three axes through servo control.

Standard

Fuel and Oil Quantity Instruments

2012-08-22

CURRENT

AS405D

This Aeronautical Standard covers two basic types of instruments as follows: Type I - Float Instruments Type II - Capacitance Instruments

Standard

Flight Directors (Reciprocating Engine Powered Aircraft)

2011-08-10

HISTORICAL

AS420A

This Aerospace Standard establishes essential minimum safe performance standards for Flight Director instruments primarily for use with reciprocating engine powered transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. This Aerospace Standard covers Flight Directors for use on aircraft to indicate to the pilot, by visual means, the correct control application for the operation of an aircraft in accordance with a pre-selected flight plan.

Standard

FLIGHT TEST PROCEDURES FOR STATIC PRESSURE SYSTEMS INSTALLED IN SUBSONIC TRANSPORT AIRCRAFT

2011-08-10

HISTORICAL

ARP921

This Aerospace Recommended Practice covers the test procedures and equipment for performing flight testing on pitot-static systems installed in subsonic transport type aircraft.

Standard

THERMO-SENSITIVE ELEMENT (RESISTANCE BULB TYPE)

2008-02-16

CURRENT

AS234

Standard

THERMO-SENSITIVE ELEMENT (IRON - CONSTANTAN)

2008-02-16

CURRENT

AS196

Standard

Airstream Deviation Instrument (ADI)

2008-02-16

CURRENT

ARP794A

This recommended practice covers an instrument which measures and displays angle of deviation of the airstream dependent on mounting location on the aircraft.

Standard

COMPASS, MAGNETIC, NON-STABILIZED TYPE (FOR TURBINE-POWERED, SUBSONIC AIRCRAFT)

2008-02-16

CURRENT

AS443A

This SAE Aerospace Standard (AS) covers a direct reading magnetic compass.

Standard

Stall Warning Instrument (Turbine Powered Subsonic Aircraft)

2008-02-16

CURRENT

AS439A

This standard covers stall warning instruments to provide positive warning to the pilot of an impending stall. Stall, as defined for the purpose of this standard, is the minimum steady flight speed at which the airplane is controllable.

Standard

RATE OF CLIMB INDICATOR, PRESSURE ACTUATED (VERTICAL SPEED INDICATOR)

2008-02-16

CURRENT

AS394A

This Aeronautical Standard covers four (4) basic types of direct indicating instruments as follows: TYPE I - Range 0-2000 feet per minute climb and descent TYPE II - Range 0-3000 feet per minute climb and descent TYPE III - Range 0-4000 feet per minute climb and descent TYPE IV - Range 0-6000 feet per minute climb and descent

Standard

AIRSPEED INDICATOR (PITOT STATIC) (RECIPROCATING ENGINE POWERED AIRCRAFT)

2008-02-16

CURRENT

AS391C

This Aeronautical Standard covers five basic types of airspeed instruments as follows:

Standard

Temperature Instruments (Reciprocating Engine Powered Aircraft)

2008-02-16

CURRENT

AS413B

This Aerospace Standard covers two basic types of temperature instruments as follows: TYPE I: Ratiometer type, actuated by changes in electrical resistance of a temperature sensing electrical resistance element; the resistance changes being obtained by temperature changes of the temperature sensing resistance element. TYPE II: Millivoltmeter type, operated and actuated by varying E.M.F. output of a thermocouple; the varying E.M.F. input to the instrument being obtained by temperature changes of the temperature sensing thermocouple.

Standard

TEMPERATURE INSTRUMENTS (TURBINE POWERED SUBSONIC AIRCRAFT)

2008-02-16

CURRENT

AS414B

This SAE Aerospace Standard (AS) covers two basic types of temperature instruments as follows: Type I: Ratiometer type, actuated by changes in electrical resistance of a temperature sensing electrical resistance element; the resistance changes being obtained by temperature changes of the temperature sensing resistance element. Type II: Millivoltmeter type, operated and actuated by varying EMF output of a thermocouple; the varying EMF input to the instrument being obtained by temperature changes of the temperature sensing thermocouple.

Standard

Air Data Computers, MPS

2008-02-16

CURRENT

AS417A

This Standard covers air data equipment (hereinafter designated the instrument) which when connected to sources of aircraft electrical power, static pressure, total pressure and outside air temperature (singly or in combination) provides some or all of the following computed air data output signals: Pressure Altitude* Total Temperature* Pressure Altitude (Reporting) Altitude Rate Baro-Corrected Pressure Altitude* Overspeed Warning Vertical Speed* Altitude Hold Computed Airspeed* Airspeed Hold Mach Number* Mach Hold Maximum Allowable Airspeed* qc (impact pressure) Static Air Temperature (*when used as an alternate for total temperature) True Airspeed Others

Standard

Flight Directors (Reciprocating Engine Powered Aircraft)

2008-02-16

CURRENT

AS420B

This Aerospace Standard covers Flight Directors for use on aircraft to indicate to the pilot, by visual means, the correct control application for the operation of an aircraft in accordance with a pre-selected flight plan.